US2072693A - Hydraulic control apparatus - Google Patents
Hydraulic control apparatus Download PDFInfo
- Publication number
- US2072693A US2072693A US712679A US71267934A US2072693A US 2072693 A US2072693 A US 2072693A US 712679 A US712679 A US 712679A US 71267934 A US71267934 A US 71267934A US 2072693 A US2072693 A US 2072693A
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- Prior art keywords
- diaphragm
- pipeline
- thermostat
- hydraulic
- piston
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K31/00—Actuating devices; Operating means; Releasing devices
- F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
- F16K31/126—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a diaphragm, bellows, or the like
Definitions
- This invention relates to hydraulic control apparatus and has particular reference to such apparatus in which movement or energy is required to be transmitted over a considerable distance.
- An object of the invention is to render such systems virtually immune from ill effects of temperature change in the whole system.
- a further object is to render such systems immune from temperature change in any part or parts of the system.
- a further object of the invention is to enable a hydraulic system readily to be adjusted either by an operator or by thermostatic means.
- the invention consists broadly in the provision, in combination with a hydraulic pipeline in energy or movement-transmitting apparatus'with what I term a shadow line, or any other hydraulically operated thermostat element which will be sensitive to the same temperature changes as those which may be expected to affect the main pipeline; and the invention provides means whereby a hydraulic thermostat element is adapted to influence the effective volumetric content of the main pipeline and. associated parts, whereby such volume may be'increased or decreased, or kept constant in accordance with temperature change.
- the invention can be seen from the accompanying drawings, in which it is shown in various adaptations. 3
- Figure 1 diagrammaticallyillustrates the invention as applied to a simply conceived hydraulic system. This figure is purely diagrammatic for the purpose of demonstrating the underlying idea of the invention
- FIG. 2 is a similar figure illustrating a slight variation or elaboration of the same'idea
- Figure 3 illustrates a detail of a-further varia- Figure 4 illustrates a practical application of the device to a petrol cock operating apparatus
- a hydraulic move- 65 ment or energy-transmitting apparatus comprises by means of a lever 5 on a spindle B with any suitable screw thread or inclined plane device indicated at l.
- The. chamber 3 is similarly closed by a diaphragm.8 which has directly connected with it an operated element 9; the distance of which in relation to a fixed point 10 is shown diagrammatically.
- the main pipe I has a branch I connecting it to a compensating chamber I2 again closed by a deformable diaphragm 13.
- the wall of the chamber l2 forms a part of a rigid structure which at its upper end carries another chamber M with a deformable diaphragm wall IS.
- a rigid arrangement comprising two cross heads I6 is interconnected by rods H.
- the cross heads l6 both bear downwards on the diaphragms I3 and I5, and they are urged towards the diaphragms by the compression spring 3 which resides between the bottom rigid wall of the chamber l4 and the lower cross head IS.
- the chamber I4 is connected with a secondary pipeline it which puts its contents in connection with a thermostat capsule 20.
- the capsule 20 is so positioned and constituted as to be sensitive to the same variations of temperature as the main pipe .I. It is preferred that the volume of the capsule 2
- the volume of the thermostat system and halving the eifectiveoarea ot'its diaphragm I5, or perhaps the volumes may be chosen having regard to some differences 0! temperature which must inevitably exist (owing to special circumstance) between the thermostat and the pipeline tobe compensated.
- the operation of the device will be fairly obvious; the pipeline l and chambers? and 3 simply -form a'remote .hydraulic movement or energy transmitter operated by handle 5 and varying the distance between 9 and I0. Let it be assumed that the atmospheric temperature rises and consequently the liquid in this system expands. Were it not for compensation the distance between 9 and I would clearly be diminished; but the liquid in i4, i9, 20 is assumed equally to expand.
- the capsule 28 takes the form of what I call a shadow pipeline, which closely follows the layout of the pipe I in propinquity therewith, then any local temperature disturbance, apart from an overall disturbance, will be compensated just as effectively.
- the main pipeline I interconnects cylinders, 22 and 23 in which operate pistons 24 and 25 respectively, the pistons being held up to the liquid by compression springs 24A, 25A respectively and being on the one hand operated by rod 243 and lever 24C, and operating on the other hand by rod 25B and lever 25C.
- the pipe I' has a branch 2
- a compression spring 30 bears on the piston 29 in the upper part of the cylinder, which again has a breather hole 26A at the top.-
- the upper part of the cylinder 26 has a pipe connection 3I to a thermostat capsule 32.
- the spring 38 holds the piston 29 on to the thermostat liquid, and the position of this piston of course determines the position of the piston 21 and therefore the efiective volumetric capacity of the main hydraulic system I, 22, 23.
- the spring 30 or equivalent loading should exert a pressure in excess of that expected in the hydraulic system having regard to the assistance it may receive from atmospheric pressure.
- FIG 3 shows diagrammatically a variant in which a differential piston is used for compensation.
- the main pipeline I is connected by a branch 2
- the cylinder 33 has working in it a plunger 31 with an upward extension which carries an annular piston head 38 working in the cylinder 34.
- the effective area of the piston 38 in relation to that of the piston 31 is prescribed according to the relative volumetric capacities of the themestat system 35, 36, and the main hydraulic system I and auxiliary parts.
- the remaining Figure 4 shows a practical application of the device to a petrol cock operating apparatus intended for use in aircraft where remote control is desired, together with precision of operation and freedom from temperature effect.
- the device consists broadly in a generator '(A), a motor actuated cock or valve (13) and a thermal compensator union (C). These parts are interconnected by apipeline and branch such as land II of Figure 1, and the union of .C is of course connected to a thermostat capsule or shadow pipeline 83.
- the operative element or generator of A comprises a chamber having two mutually bolted halves M, 42 between which is secured the edge of a disc-like deformable diaphra'gm 43 which divides the chamber. The.
- FIG. B illustrates a petrol-cock or valve in a main petrol line indicated by the conduit 52 with unions 53 formed on a suitable body 54.
- the conduit 52 has through connection,through a diagonal wall 55 pierced by a port 56 with a knife or other valve seat 51 on which seats a disc valve 58 with any suitable seal such as a leather annular insert 59.
- the valve 58 is mounted on a sliding stem 60 mounted in suitable bearings at 6
- the member 66 has a suitable union at 61 for connection with the pipeline I.
- a compression spring 68 urges the diaphragm 65, stem 68 and valve 58 in the direction to seat and close the valve. It is of course assumed that the whole space of the system between the diaphragms 43 of A and 65 of B is completely filled with liquid of suitable nature. Now rotation of the lever 49, by appropriate movement of the diaphragm 43, will cause movement of the diaphragm 65 by hydraulic pressure and may thus be used to open or close the valve 58. In the event of a crash or other cause of pipeline breakage the hydraulic pressure will fail and the valve 58 will therefore close. If it it be so desired, the spring influence on the system maybe reversed so that in the event of a pipeline failure the valve 58 will open.
- secures by its edges a diaphragm 12 to a body rigidly constituted and indicated by the parts 13.
- This rigid body carries another cover plate 14 similar to II with a union at connecting it to shadow pipeline or thermostat capsule 83.
- the plate 14 together with a deformablediaphragm 16 forms an adjusting chamber affected by the temperature conditions ofthe thermostat.
- Connected to the diaphragm 12 is'a cross head 11 which is connected in turn by rigid rods 18 to a second cross head 19 which is connected to the diaphragm 16. Between a fixed part of the body 13 and the cross head 11, and surrounding the rods 18, are compression springs 88.
- these springs have the effect of keeping the diaphragm 16 in compression on the thermostat liquid, but by yielding or expanding they allow the cross head 11 to follow the, movements of the diaphragm 16.; thus the diaphragm 12 is governed by the diaphragm 16 and consequently the effective volumetric capacity of the hydraulic system connected by the union 10 is likewise controlled.
- the springs 89 in their cumulative effect should not be less than the maximum working pressure to which the diaphragm 12 will be subjected. In some cases it may be convenient to employ a further compression spring 81 below the diaphragm 12 opposing the springs 89.
- is a. light compresaovaoes sion spring provided to urge the diaphragm 12 against the cross head 11 particularly when the system is empty.
- thermostat system above described be filled with characteristically eimner liquid to the working system, or, one of which the physical characteristics either are or can effectively be made the same as that of the operating liquid, For example, a liquid with a less coefflcient of expansion may be used, providing the effective volume is increased.
- a hydraulic system for the transmission of force to a remote point comprising a liquid-filled I force transmission line having at one point operating means for applying pressure to the liquid in the line and at another point operable means responsive to pressure variations in said line,-
- auxiliary line independent oi'said operating and operable means, said auxiliary line being positioned alongside said iorce transmission line and being substantially co-extenslve therewith, and a pressure sensitive element in said auxiliary line connected to said capacity changing means to actuate the same in response to temperature variations in said line.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Temperature-Responsive Valves (AREA)
Description
March 2, 1937. s. R. VOLKERT 2,072,693
HYDRAULIC CONTROL APPARATUS Filed Feb. 23, 1934 2 Sheets-Sheet l INVENTOR WWW ATTORNEYS.
s. R. VOLKERT 2,072,693
Filed Feb. 23, 1934 2 Sheets-Sheet 2 March 2, 1937.
nymuumc CONTROL APPARATUS INVENTOR ATTORNEYS 45 tion diagrammatically;
I Patented ar. 2, i937 orricr signor of one-half to Automotive Pr pany Limited, London, England oducts Com- Appiication February 23, 1934, Serial No. 712,679 In Great Britain February 23, 1933 1 Claim.
This invention relates to hydraulic control apparatus and has particular reference to such apparatus in which movement or energy is required to be transmitted over a considerable distance.
An object of the invention is to render such systems virtually immune from ill effects of temperature change in the whole system. A further object is to render such systems immune from temperature change in any part or parts of the system. In this connection it is observed that in certain circumstances, for example in aircraft installations, one part of a pipeline may be rapidly cooled, whereas another part may be rapidly heated simultaneously, and the problem of thermostatic control-of expansion and contraction is thus a far from straightforward one.
A further object of the invention is to enable a hydraulic system readily to be adjusted either by an operator or by thermostatic means.
With-this and other objects in view the invention consists broadly in the provision, in combination with a hydraulic pipeline in energy or movement-transmitting apparatus'with what I term a shadow line, or any other hydraulically operated thermostat element which will be sensitive to the same temperature changes as those which may be expected to affect the main pipeline; and the invention provides means whereby a hydraulic thermostat element is adapted to influence the effective volumetric content of the main pipeline and. associated parts, whereby such volume may be'increased or decreased, or kept constant in accordance with temperature change. The invention can be seen from the accompanying drawings, in which it is shown in various adaptations. 3
Figure 1 diagrammaticallyillustrates the invention as applied to a simply conceived hydraulic system. This figure is purely diagrammatic for the purpose of demonstrating the underlying idea of the invention;
' Figure 2 is a similar figure illustrating a slight variation or elaboration of the same'idea;
Figure 3 illustrates a detail of a-further varia- Figure 4 illustrates a practical application of the device to a petrol cock operating apparatus,
in which Aillustrates a sectional elevation or plan of an operating element adapted for the particular purpose of operating a remotely posi-" tionedpetrol cock; 3 being a similar view of the 2 petrol cock; and C is a partly sectioned elevation of a thermostatically controlling device.
Referring now to Figure 1, a hydraulic move- 65 ment or energy-transmitting apparatus comprises by means of a lever 5 on a spindle B with any suitable screw thread or inclined plane device indicated at l. The. chamber 3 is similarly closed by a diaphragm.8 which has directly connected with it an operated element 9; the distance of which in relation to a fixed point 10 is shown diagrammatically. The main pipe I has a branch I connecting it to a compensating chamber I2 again closed by a deformable diaphragm 13. The wall of the chamber l2 forms a part of a rigid structure which at its upper end carries another chamber M with a deformable diaphragm wall IS. A rigid arrangement comprising two cross heads I6 is interconnected by rods H. The cross heads l6 both bear downwards on the diaphragms I3 and I5, and they are urged towards the diaphragms by the compression spring 3 which resides between the bottom rigid wall of the chamber l4 and the lower cross head IS. The chamber I4 is connected with a secondary pipeline it which puts its contents in connection with a thermostat capsule 20. Although not so illustrated diagrammatically, the capsule 20 is so positioned and constituted as to be sensitive to the same variations of temperature as the main pipe .I. It is preferred that the volume of the capsule 2|], pipe l9 and chamber I4 is equal to or thermally equivalent to the volume of the chambers 2 and 3 and the pipeline I. It need hardly be men tioned, however, that these volumes may. be proportionated by, for example, halving the volume of the thermostat systemand halving the eifectiveoarea ot'its diaphragm I5, or perhaps the volumes may be chosen having regard to some differences 0! temperature which must inevitably exist (owing to special circumstance) between the thermostat and the pipeline tobe compensated. The operation of the device will be fairly obvious; the pipeline l and chambers? and 3 simply -form a'remote .hydraulic movement or energy transmitter operated by handle 5 and varying the distance between 9 and I0. Let it be assumed that the atmospheric temperature rises and consequently the liquid in this system expands. Were it not for compensation the distance between 9 and I would clearly be diminished; but the liquid in i4, i9, 20 is assumed equally to expand. and this causes the diaphragm ii to deform outwardly so that the cross heads and rods l6, l1 rise .and either allow to distort or actually efl'e'ct distortion or the diaphragm l3, so that the expansion of operating fluid is precisely accommodated and therefore compensated. If, as preferred, the capsule 28 takes the form of what I call a shadow pipeline, which closely follows the layout of the pipe I in propinquity therewith, then any local temperature disturbance, apart from an overall disturbance, will be compensated just as effectively. a
Turning now to Figure 2, a slight variation of construction, but not of essential principle, is shown, and like parts .are numbered alike. The main pipeline I interconnects cylinders, 22 and 23 in which operate pistons 24 and 25 respectively, the pistons being held up to the liquid by compression springs 24A, 25A respectively and being on the one hand operated by rod 243 and lever 24C, and operating on the other hand by rod 25B and lever 25C. The pipe I'has a branch 2| lead-- ing to a third cylinder 26 with a breather hole at 26A and having a piston 21 connected to a piston rod 28 and, thereby, to another piston 29 operating in an extension of the cylinder 26 through the bottom wall thereof. A compression spring 30 bears on the piston 29 in the upper part of the cylinder, which again has a breather hole 26A at the top.- The upper part of the cylinder 26 has a pipe connection 3I to a thermostat capsule 32. In general the same remarks apply to this system as to that of Figure 1, the difference residing in the piston and cylinder arrangement rather than the deformable diaphragm arrangement. It will be observed that the spring 38 holds the piston 29 on to the thermostat liquid, and the position of this piston of course determines the position of the piston 21 and therefore the efiective volumetric capacity of the main hydraulic system I, 22, 23. In all such cases the spring 30 or equivalent loading should exert a pressure in excess of that expected in the hydraulic system having regard to the assistance it may receive from atmospheric pressure.
Figure 3 shows diagrammatically a variant in which a differential piston is used for compensation. In this case the main pipeline I is connected by a branch 2| to a lower cylinder 33 which has a coaxial upper cylinder extension 34 with a pipe connection 35 to the thermostat capsule 36. The cylinder 33 has working in it a plunger 31 with an upward extension which carries an annular piston head 38 working in the cylinder 34. The effective area of the piston 38 in relation to that of the piston 31 is prescribed according to the relative volumetric capacities of the themestat system 35, 36, and the main hydraulic system I and auxiliary parts.
The remaining Figure 4 shows a practical application of the device to a petrol cock operating apparatus intended for use in aircraft where remote control is desired, together with precision of operation and freedom from temperature effect. The device consists broadly in a generator '(A), a motor actuated cock or valve (13) and a thermal compensator union (C). These parts are interconnected by apipeline and branch such as land II of Figure 1, and the union of .C is of course connected to a thermostat capsule or shadow pipeline 83. The operative element or generator of A comprises a chamber having two mutually bolted halves M, 42 between which is secured the edge of a disc-like deformable diaphra'gm 43 which divides the chamber. The. diaphragm' 43 ,is secured by suitable washers or collars 44 to an axially movable and rotatable spindle 45 which has a radialpin at 46 to cooperate with a fixed inclined edge or cam 41 with preferably a dwell formed 'uponit at 48 to locate and indicate an extreme position in one direction, by restraining the movements of the pin 46. The spindle 45 carries a manual lever 49, and the diaphragm 43and spindle 45 are all urged in one direction by a compression spring 58 housed between the diaphragm 43 and the casing member 42. This casing member 42 has a suitable union at for .connection to a pipeline such as I in the previous figures. It will be clear that angular movement of lever 49, by the coaction of the pin 46 and cam 41, causes axial movement of the diaphragm 43.
B illustrates a petrol-cock or valve in a main petrol line indicated by the conduit 52 with unions 53 formed on a suitable body 54. The conduit 52 has through connection,through a diagonal wall 55 pierced by a port 56 with a knife or other valve seat 51 on which seats a disc valve 58 with any suitable seal such as a leather annular insert 59. The valve 58 is mounted on a sliding stem 60 mounted in suitable bearings at 6| and 62, and attached at one end by a washer or plate 64 to a deformable. diaphragm 65 which is clamped by the edges of a casing member 66, to the body 54. The member 66 has a suitable union at 61 for connection with the pipeline I. A compression spring 68 urges the diaphragm 65, stem 68 and valve 58 in the direction to seat and close the valve. It is of course assumed that the whole space of the system between the diaphragms 43 of A and 65 of B is completely filled with liquid of suitable nature. Now rotation of the lever 49, by appropriate movement of the diaphragm 43, will cause movement of the diaphragm 65 by hydraulic pressure and may thus be used to open or close the valve 58. In the event of a crash or other cause of pipeline breakage the hydraulic pressure will fail and the valve 58 will therefore close. If it it be so desired, the spring influence on the system maybe reversed so that in the event of a pipeline failure the valve 58 will open.
C, connected to the pipeline I by union of a cover plate II is the thermostat control unit. The cover plate 1| secures by its edges a diaphragm 12 to a body rigidly constituted and indicated by the parts 13. This rigid body carries another cover plate 14 similar to II with a union at connecting it to shadow pipeline or thermostat capsule 83. The plate 14 together with a deformablediaphragm 16 forms an adjusting chamber affected by the temperature conditions ofthe thermostat. Connected to the diaphragm 12 is'a cross head 11 which is connected in turn by rigid rods 18 to a second cross head 19 which is connected to the diaphragm 16. Between a fixed part of the body 13 and the cross head 11, and surrounding the rods 18, are compression springs 88. It will be appreciated that these springs have the effect of keeping the diaphragm 16 in compression on the thermostat liquid, but by yielding or expanding they allow the cross head 11 to follow the, movements of the diaphragm 16.; thus the diaphragm 12 is governed by the diaphragm 16 and consequently the effective volumetric capacity of the hydraulic system connected by the union 10 is likewise controlled. The springs 89 in their cumulative effect should not be less than the maximum working pressure to which the diaphragm 12 will be subjected. In some cases it may be convenient to employ a further compression spring 81 below the diaphragm 12 opposing the springs 89. The spring 8| is a. light compresaovaoes sion spring provided to urge the diaphragm 12 against the cross head 11 particularly when the system is empty.
In the above specific case or in any general case of application of the invention, means may readily be provided for initial manual adjustment. For example, nuts 82 may adjust the position of cross head 19 relative to rods 18 and thus, of course, relatively adjust the diaphragms I6 and 12. By this or equivalent means the precise effective volume of the operating hydraulic system may be set. For example, if the system were too full the diaphragm I2 could be somewhat raised, or conversely. It will be clear that this and like modifications may be applied without departure from the essential scope of the invention as defined by the following claim. It must also be appreciated that the invention is applicable to divers systems; for example in treating a twopipeline hydraulic system a single shadow line may be employed in the vicinity ofboth of them,
and where I refer to an operative or hydraulic pipeline I am not restricting myself to any particular form of conduit'or number of conduits.- It
:5 is. preferred that the thermostat system above described be filled with characteristically eimner liquid to the working system, or, one of which the physical characteristics either are or can effectively be made the same as that of the operating liquid, For example, a liquid with a less coefflcient of expansion may be used, providing the effective volume is increased.
What I claim is:- A hydraulic system for the transmission of force to a remote point comprising a liquid-filled I force transmission line having at one point operating means for applying pressure to the liquid in the line and at another point operable means responsive to pressure variations in said line,-
means connected to said line for changing the volumetric capacity thereof, a closed liquid-filled auxiliary line independent oi'said operating and operable means, said auxiliary line being positioned alongside said iorce transmission line and being substantially co-extenslve therewith, and a pressure sensitive element in said auxiliary line connected to said capacity changing means to actuate the same in response to temperature variations in said line.
GEORGE RUDOLPH VOLKERT.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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GB2072693X | 1933-02-23 |
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US2072693A true US2072693A (en) | 1937-03-02 |
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US712679A Expired - Lifetime US2072693A (en) | 1933-02-23 | 1934-02-23 | Hydraulic control apparatus |
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Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2417256A (en) * | 1943-08-20 | 1947-03-11 | Adel Prec Products Corp | Compensator-accumulator unit for hydraulic systems |
US2421866A (en) * | 1942-12-24 | 1947-06-10 | Scott Aviation Corp | Compressor for hydraulic brake units and the like |
US2427591A (en) * | 1942-11-20 | 1947-09-16 | Jr William C Denison | Hydraulic apparatus |
US2449392A (en) * | 1945-05-25 | 1948-09-14 | Adel Prec Products Corp | Pulsator system |
US2536628A (en) * | 1944-03-28 | 1951-01-02 | West Road Co Ltd | Transmission line and temperature compensating means for hydraulic systems |
US2575319A (en) * | 1946-06-17 | 1951-11-13 | Merit Engineering Inc | Hydraulic transmitter |
US2580561A (en) * | 1945-09-10 | 1952-01-01 | Link Belt Co | Hydraulic pulsator transmission system for converting rotary motion into reciprocatory motion |
US2592221A (en) * | 1943-07-27 | 1952-04-08 | Stewart Warner Corp | Fluid stabilizing means for hydraulic control systems |
US2626106A (en) * | 1948-02-09 | 1953-01-20 | Honeywell Regulator Co | Control apparatus |
US2789845A (en) * | 1953-06-10 | 1957-04-23 | Karl A Klingler | Journal box seal |
US2941404A (en) * | 1954-12-24 | 1960-06-21 | Standard Thomson Corp | Ambient-compensated actuator |
US3036777A (en) * | 1956-09-27 | 1962-05-29 | American Radiator & Standard | Adjustable thermal mixing valve |
US3203186A (en) * | 1960-08-25 | 1965-08-31 | Edwin J Lukas | Force transmitting system |
US4372118A (en) * | 1976-10-26 | 1983-02-08 | Andresen Herman J | Liquid cable |
US4946329A (en) * | 1988-04-01 | 1990-08-07 | Albert Einstein College Of Medicine Of Yeshiva University | Micromanipulator using hydraulic bellows |
US6098405A (en) * | 1995-12-18 | 2000-08-08 | Nippon Zeon Co., Ltd. | Drive unit for medical equipment |
-
1934
- 1934-02-23 US US712679A patent/US2072693A/en not_active Expired - Lifetime
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2427591A (en) * | 1942-11-20 | 1947-09-16 | Jr William C Denison | Hydraulic apparatus |
US2421866A (en) * | 1942-12-24 | 1947-06-10 | Scott Aviation Corp | Compressor for hydraulic brake units and the like |
US2592221A (en) * | 1943-07-27 | 1952-04-08 | Stewart Warner Corp | Fluid stabilizing means for hydraulic control systems |
US2417256A (en) * | 1943-08-20 | 1947-03-11 | Adel Prec Products Corp | Compensator-accumulator unit for hydraulic systems |
US2536628A (en) * | 1944-03-28 | 1951-01-02 | West Road Co Ltd | Transmission line and temperature compensating means for hydraulic systems |
US2449392A (en) * | 1945-05-25 | 1948-09-14 | Adel Prec Products Corp | Pulsator system |
US2580561A (en) * | 1945-09-10 | 1952-01-01 | Link Belt Co | Hydraulic pulsator transmission system for converting rotary motion into reciprocatory motion |
US2575319A (en) * | 1946-06-17 | 1951-11-13 | Merit Engineering Inc | Hydraulic transmitter |
US2626106A (en) * | 1948-02-09 | 1953-01-20 | Honeywell Regulator Co | Control apparatus |
US2789845A (en) * | 1953-06-10 | 1957-04-23 | Karl A Klingler | Journal box seal |
US2941404A (en) * | 1954-12-24 | 1960-06-21 | Standard Thomson Corp | Ambient-compensated actuator |
US3036777A (en) * | 1956-09-27 | 1962-05-29 | American Radiator & Standard | Adjustable thermal mixing valve |
US3203186A (en) * | 1960-08-25 | 1965-08-31 | Edwin J Lukas | Force transmitting system |
US4372118A (en) * | 1976-10-26 | 1983-02-08 | Andresen Herman J | Liquid cable |
US4946329A (en) * | 1988-04-01 | 1990-08-07 | Albert Einstein College Of Medicine Of Yeshiva University | Micromanipulator using hydraulic bellows |
US6098405A (en) * | 1995-12-18 | 2000-08-08 | Nippon Zeon Co., Ltd. | Drive unit for medical equipment |
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